IP Library › Granted Patent US 11,560,899
Granted Patent B2
US 11,560,899 · App. 17/282,395 · Granted Jan 24, 2023

Pump with axially-elongated annular seal element between inducer and impeller

Inventors: Jeff Miller (Simi Valley, CA); Steven Grota (Sacramento, CA)
Assignee: AEROJET RICKETDYNE, INC.
F04D29/22
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,560,899
App. No.
17/282,395
Granted
Jan 24, 2023
Kind
B2
Abstract

A pump includes a shaft that is rotatable about a central axis. An inducer is mounted on the shaft and has an inducer blade and inducer shroud attached at an outer end of the inducer blade. An impeller is mounted on the shaft downstream of the inducer and has an impeller blade and an impeller shroud attached at an outer end of the impeller blade. There is an axially-elongated annular seal element disposed at an axial end of the inducer shroud that provides sealing between the inducer shroud and the impeller shroud.

Claims (13)

1. A pump comprising:

a shaft rotatable about a central axis;

an inducer mounted on the shaft, the inducer having an inducer blade and an inducer shroud attached at an outer end of the inducer blade;

an impeller mounted on the shaft downstream of the inducer, the impeller having an impeller blade and an impeller shroud attached at an outer end of the impeller blade;

an axially-elongated annular seal element disposed at an axial end of the inducer shroud providing sealing between the inducer shroud and the impeller shroud, the axially-elongated annular seal element is in a flexed state such that a resiliency of the axially-elongated annular seal element provides a radial clamping force on the impeller shroud, the axially-elongated annular seal element defines an axial length and a radial thickness, and an aspect ratio of the axial length to the radial thickness is from 3 to 10.

2. The pump as recited in claim 1 , wherein the inducer shroud has an inside diameter surface that defines a passage through the inducer shroud, and the axially-elongated annular seal element is radially offset from the inside diameter surface.

3. The pump as recited in claim 1 , wherein the axially-elongated annular seal element projects axially from an enlarged base section on the inducer shroud to a free tip.

4. The pump as recited in claim 3 , wherein a distal portion of the axially-elongated annular seal element, including the free tip, is radially overlapping with the impeller shroud and a proximal portion of the axially-elongated annular seal element is non-overlapping with the impeller shroud.

5. The pump as recited in claim 4 , wherein an axial length of the distal portion that is overlapping with the impeller shroud is 25% or less of a total axial length of the axially-elongated annular seal element from the enlarged base to the free tip.

6. The pump as recited in claim 1 , wherein the axially-elongated annular seal element is formed of steel, titanium-based alloy, nickel-based alloy, aluminum, or composite.

7. The pump as recited in claim 1 , wherein the axially-elongated annular seal element is integral with the inducer shroud.

8. The pump as recited in claim 1 , wherein the inducer shroud includes a lip radially inwards of the axially-elongated annular seal element, the axially-elongated annular seal element and the lip defining an axially-extending slot in a radial space there between.

9. The pump as recited in claim 8 , wherein the lip is spaced from an axial edge of the impeller shroud.

Assignments (3)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 064423/0966 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Sep 28, 2022
From: AEROJET ROCKETDYNE, INC.
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 061561/0451 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 2, 2021
From: MILLER, JEFF; GROTA, STEVEN
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 055804/0410 →
Continuity (1)
Related Publication 20210340989A1 · Nov 4, 2021